EP2410186B1 - Roue et machine rotative - Google Patents

Roue et machine rotative Download PDF

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Publication number
EP2410186B1
EP2410186B1 EP10799530.0A EP10799530A EP2410186B1 EP 2410186 B1 EP2410186 B1 EP 2410186B1 EP 10799530 A EP10799530 A EP 10799530A EP 2410186 B1 EP2410186 B1 EP 2410186B1
Authority
EP
European Patent Office
Prior art keywords
impeller
blade
hub
bulge
flow passage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP10799530.0A
Other languages
German (de)
English (en)
Other versions
EP2410186A1 (fr
EP2410186A4 (fr
Inventor
Jo Masutani
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of EP2410186A1 publication Critical patent/EP2410186A1/fr
Publication of EP2410186A4 publication Critical patent/EP2410186A4/fr
Application granted granted Critical
Publication of EP2410186B1 publication Critical patent/EP2410186B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30—Vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/286—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors

Definitions

  • the present invention relates to an impeller and a rotary machine, and particularly, to a flow passage shape thereof.
  • impellers for example, refer to JP-A-2005-163640 and JP-A-2005-180372 ) in which turbulence is caused in a flow along the hub surface by forming a plurality of grooves in the hub surface between blades such that a boundary layer of the flow along the hub surface is not expanded, in order to improve the performance of a centrifugal or mixed-flow impeller, and in which a plurality of small blades is provided between blades in order to prevent local concentration of a boundary layer.
  • US 5,215,439 discloses a centrifugal impeller with a hub formed about an axis of rotation with a plurality of substantially radially extending blades affixed to the hub. Each blade has a suction surface, and a pressure surface formed on the adjacent blade facing the suction surface. A portion of the hub extends towards the outside which leads to improve the flow characteristics over impellers having concentric hub configurations.
  • KR 2003-0033881 A represents the closest prior art document.
  • FIG. 9 shows the vicinity of a leading edge of a blade in a related-art impeller.
  • a blade angle of a blade 203 at an inlet 206 is designed so as to approach to a radial direction of the impeller relative to an entry angle (entry flow angle) of fluid to inlet 206 at a designed flow rate.
  • entry angle ⁇ the entry flow angle
  • the invention has been made in view of the above circumstances, and the object thereof is to provide an impeller and a rotary machine that can suppress a decrease in efficiency and a stall of the fluid by growing of a boudary layer on the hub surface near a suction surface n at the inlet when inflow decreases.
  • An impeller for example, the impeller 1 in the embodiment
  • An impeller is an impeller of a rotary machine in which the direction of flow gradually changes from an axial direction to a radial direction as it goes from the inside in the radial direction of a fluid flow passage (for example, the impeller flow passage 10 in the embodiment) to the outside in the radial direction thereof.
  • the impeller includes a hub surface (for example, the hub surface 4 in the embodiment) constituting at least a portion of the fluid flow passage; a blade surface (for example, the pressure surface p or the suction surface n in the embodiment) constituting at least a portion of the fluid flow passage; and a bulge (for example, the bulge b in the embodiment) that bulges toward the inside of the fluid flow passage at a corner (for example, the corner 12 in the embodiment) where a pressure surface of the blade surface comes in contact with the hub surface in the vicinity of an inlet (for example, the inlet 6 in the embodiment) of the fluid flow passage.
  • a hub surface for example, the hub surface 4 in the embodiment
  • a blade surface for example, the pressure surface p or the suction surface n in the embodiment
  • a bulge for example, the bulge b in the embodiment
  • the leading edge of the blade on the hub surface side is thickly formed and a radius of a round portion, which is formed of the bulge at the leading edge of the blade, becomes large substantively. Therefore, even when the entry angle of the fluid with respect to the blade angle becomes large because the inflow velocity on the hub surface is low, the fluid flows along the round portion, which is formed of the bulge at the leading edge of the blade and increases the radius thereof, at a slow velocity.
  • the strength of the portion contacting the blade with the hub, where a force by the fluid applies to and centrifugal stress is generated by rotating the impeller can be increased by providing a bulge at the corner in the vicinity of the inlet.
  • an increase in the number of parts can be suppressed by being formed integrally with the hub and the blade.
  • the impeller may further include a second bulge that bulges toward the inside of the fluid flow passage at a corner where a suction surface of the blade comes in contact with the hub surface in the vicinity of the inlet of the fluid flow passage.
  • the second bulge is provided at the corner where the suction surface of the blade comes in contact with the hub surface in addition to the bulge that is provided at the corner where the pressure surface of the blade surface comes in contact with the hub surface, the thickness of the leading edge of the blade near the hub surface can be larger. Therefore, it is possible to further suppress the growing of a boundary layer due to decreases in the flow rate, and the strength of the portion contacting the blade with the hub in the vicinity of the inlet can be further increased.
  • the impeller of the rotary machine related to the invention even when the entry angle of the fluid with respect to the blade angle becomes large when the flow rate is low, enlarging a boundary layer at the inlet (in particular, on the hub surface near the suction surface) can be suppressed, depending on the increase in the radius of the leading edge of the blade, by providing the bulge thereon. Therefore, there is an advantage that a decrease in the efficiency of the low flow rate and the stall of the fluid can be suppressed.
  • a centrifugal compressor 100 that is a rotary machine of the present embodiment, as shown in FIG. 1 is mainly constituted by, as an example, a shaft 102 that is rotated around an axis O, an impeller 1 that is attached to the shaft 102 and compresses process gas (gas) G using a centrifugal force, and a casing 105 that rotatably supports the shaft 102 and is formed with a flow passage 104 that allows the process gas G to pass from the upstream to the downstream.
  • a casing 105 is formed so as to form a substantially columnar outline, and the shaft 102 is arranged so as to pass through a center.
  • Journal bearings 105a are provided at both ends of the shaft 102 in an axial direction, and a thrust bearing 105b is provided at one end.
  • the journal bearings 105a and the thrust bearing 105b rotatably support the shaft 102. That is, the shaft 102 is supported by the casing 105 via the journal bearings 105a and the thrust bearing 105b.
  • a suction port 105c into which the process gas G is made to flow from the outside is provided on the side of one end of the casing 105 in the axial direction, and a discharge port 105d through which the process gas G flows to the outside is provided on the side of the other end.
  • suction port 105c and the discharge port 105d communicate with each other via the impeller 1 and the flow passage 104.
  • a plurality of the impellers 1 is arranged at intervals in the axial direction of the shaft 102.
  • six impellers 1 are provided in the illustrated example, it is only necessary that at least one or more impellers are provided.
  • FIGS. 2 to 3 show the impeller 1 of the centrifugal compressor 100, and the impeller 1 includes a hub 2 and a plurality of blades 3.
  • the hub 2 is formed in a substantially round shape in front view, and is made rotatable around the axis with the axis O as a center.
  • a hub surface 4 is formed so as to be curved toward the outside in the radial direction from a predetermined position S on the inside in the radial direction slightly separated radially outward from the axis O.
  • This curvedly formed hub surface 4 is formed such that a surface located on the inside in the radial direction is formed along the axis O, and runs along the radial direction gradually as it goes to the outside in the radial direction.
  • the hub 2 is formed such that the axial thickness thereof decreases from one (upstream) of the axial end surfaces as it goes to the outside in the radial direction from the position S on the inside in the radial direction slightly separated from the axis O, and this axial thickness becomes larger near the inside and becomes smaller near the outside.
  • an arrow indicates the radial direction of the hub 2.
  • a plurality of blades 3 is substantially radially arranged on the above-described hub surface 4 as shown in FIG. 2 , and is erected substantially perpendicularly (in normal direction) to the hub surface 4 as shown in FIG. 4 .
  • the blade 3 is formed such that the thickness thereof is substantially uniform from a hub end h up to a tip end t, and shows a curved shape that slightly becomes a convex surface toward the rotational direction (shown by an arrow in FIG. 2 ) of the hub 2 from the hub end h (refer to FIG. 3 ) to the tip end t.
  • a blade surface on a convex side of respective blade surfaces on a convex side and the convex side of the curved blade 3 becomes a pressure surface p
  • a blade surface on the concave side that is a back side of the convex surface becomes the suction surface n.
  • the tip end t of a blade 3 is formed so as to be curved from the inside in the radial direction of the hub 2 to the outside in the radial direction thereof. More specifically, similarly to the above-described hub surface 4, the blade is formed in a concave shape that runs along the axis O nearer the inside in the radial direction and runs along the radial direction gradually as it goes to the outside in the radial direction.
  • the blade 3 is formed so as to be higher near the inside in the radial direction of the hub 2 and lower near the outside in the radial direction thereof.
  • an impeller flow passage 10 of the impeller 1 is constituted by a shroud surface 5 constituted by the casing 105, the pressure surface p and suction surface n of adjacent blades 3 described above, and the hub surface 4 between the pressure surface p and the suction surface n.
  • a fluid flows in along the radial direction from an inlet 6 of the impeller flow passage 10 located on the inside in the radial direction of the hub 2, and the fluid flows out to the outside along the radial direction from an outlet 7 located on the outside in the radial direction due to a centrifugal force.
  • the impeller flow passage 10 having the configuration described above is formed so as to be curved from the above-described inlet 6 toward the outlet 7, and the direction of flow of the flow passage gradually changes from the axial direction to the radial direction as it goes from the inside in the radial direction of the hub 2 to the outside in the radial direction thereof.
  • a bulge b that bulges toward the inside of the impeller flow passage 10 is formed at a corner 12 where the hub surface 4 comes in contact with the pressure surface p of the blade 3 in the vicinity of an inlet 6.
  • the bulge b is formed integrally with the hub surface 4 and the pressure surface p (refer to FIGS. 2 to 4 ).
  • a cross-sectional shape of the leading edge 20 of the blade 3 is formed in a substantially semicircular shape (refer to FIG. 5 ).
  • the bulge b is formed at the corner 12 in the vicinity of the inlet 6 in the above-desciribed corner 12 (that is, a part of the corner 12 nearby the leading edge 20).
  • the maximum width of the bulge b is set to about 20% of the width of the impeller flow passage 10, and to about 20% of the height of the blade 3.
  • the bulge b has a maximum width and a maximum height at a position where the bulge b smoothly bulges as it goes along a flow direction from a vicinity of the inlet 6 to downstream in a curved surface protruding toward the inside of the impeller flow passage 10.
  • the bulge b gradually decreases in the curved surface same as the above from the position having the maximum width and the maximum height, and smoothly connects to the hub surface 4 and the pressure surface p at a position of about 10% of the flow passage length from the inlet 6 to the outlet 7 of the impeller flow passage 10.
  • the thickness of the leading edge 20 of the blade 3 near the hub surface 4 is increased by forming the bulge b in this manner, and the radius r1 of the leading edge of the blade practically increases to the radius r2 of the leading edge of the blade as shown in FIG. 5 .
  • FIG. 6 is a graph showing the efficiency characteristics of rotary machines using the impeller 1 and a related-art impeller.
  • the vertical axis represents efficiency ⁇
  • the horizontal axis represents flow rate Q.
  • a solid line shows the efficiency of a rotary machine including an impeller that is not provided with the bulge b
  • a broken line shows the efficiency of a rotary machine including the above-described impeller 1 that is provided with the bulge b.
  • FIG. 7 is a graph showing the head (work) characteristics of the rotary machines using the impeller 1 and the related-art impeller, and the vertical axis represents head (work), and the horizontal axis represents the flow rate Q.
  • a solid line shows the head of a rotary machine including an impeller that is not provided with the bulge b
  • a broken line shows the head of a rotary machine including the above-described impeller 1 that is provided with the bulge b.
  • a surge point (shown by an open circle in the drawing) of the rotary machine including the above-described impeller 1 that is provided with the bulge b is displaced toward a lower flow rate side more than a surge point of the rotary machine including the impeller that is not provided with the bulge b (shown by a filled circle in the drawing), and a surge margin is expanded.
  • the reason why the efficiency characteristics of the impeller 1 is improved and the surge point is displaced toward a lower flow rate side in comparison with the impeller without the bulge b is that it is difficult to grow a boundary layer on the suction surface n by partial increasing of the radius of the leading edge of the blade at the inlet 6 in a case where the entry angle of the fluid as shown in FIG. 2 becomes large when a flow rate is low.
  • the surge point is a minimum flow rate at which a rotary machine is required to operate normally without surging.
  • the thickness of the leading edge 20 of the blade 3 near the hub surface 4 is partially increased by providing the bulge b at the corner 12 where the hub surface 4 comes in contact with the pressure surface p in the vicinity of the inlet 6. Therefore, the radius r1 of the leading edge of the blade near the hub surface 4 practically increases to the radius r2 of the leading edge of the blade, and growing of a boundary layer on the suction surface near the hub at a designed flow rate can be suppressed.
  • the radius r1 of the leading edge of the blade practically increases to the radius r2 of the leading edge of the blade by forming the leading edge 20 of the blade 3 near the hub surface 4 to be thick with the bulge b, even when the entry angle of the fluid with respect to the blade angle (refer to FIG. 2 ) becomes large, enlarging a boundary layer on the hub surface 4 near the suction surface n can be suppressed.
  • suppressing a decrease in the efficiency at low flow rate and preventing from the stall of the fluid can be achieved, and the surge margin can be expanded.
  • the strength of the portion contacting the blade 3 with the hub 2, where a force by the fluid applies to and centrifugal stress is generated by high-speed rotating the impeller 1, can be increased by providing the bulge b at the corner 12 in the vicinity of the inlet 6.
  • an increase in the number of parts can be suppressed by being formed integrally with the hub 2 and the blade 3.
  • the bulge b' may be provided at the corner 22 where the suction surface n comes in contact with the hub surface 4 in the vicinity of an inlet 6 of the fluid flow passage 10.
  • the bulge b' since the thickness of the leading edge 20 of the blade 3 near the hub surface 4 can be larger, the radius of the leading edge of the blade can further become large. Therefore, it is possible to further suppress growing of a boundary layer due to decreases in the flow rate. Moreover, the strength of the portion contacting the blade 3 with the hub 2 at the corner 12 in the vicinity of the inlet 6 can be further increased.
  • the impeller of the centrifugal rotary machine has been described in the above embodiments, the impeller is not limited to this, and may be an impeller of a mixed-flow rotary machine. Additionally, the invention may be applied to an impeller of a blower, a turbine, or the like without being limited to the compressor. Additionally, although the so-called open impeller in which the facing side of the hub surface 4 is covered with the shroud surface 5 has been described as an example in the above-described embodiment, the invention may be applied to a closed impeller including a wall that covers the tip end t side integrally formed in the blade 3.
  • the impeller of the rotary machine related to the invention even when the entry angle of the fluid with respect to the blade angle becomes large when the flow rate is low, enlarging a boundary layer at the inlet (in particular, on the hub surface near the suction surface) can be suppressed, depending on the increase in the radius of the leading edge of the blade, by providing the bulge thereon. Therefore, there is an advantage that a decrease in the efficiency of the low flow rate and the stall of the fluid can be suppressed.

Claims (3)

  1. Roue (1) d'une machine rotative (100), dans laquelle la direction d'écoulement change d'une direction axiale à une direction radiale lorsqu'elle va de l'intérieur dans la direction radiale d'un passage d'écoulement de fluide (104) à l'extérieur dans la direction radiale de celui-ci, la roue (1) comprenant :
    une surface de moyeu (4) constituant au moins une portion du passage d'écoulement de fluide (104) ;
    une pale comprenant une surface de pale constituant au moins une portion du passage d'écoulement de fluide (104) ; et
    un renflement (b) qui est renflé vers l'intérieur du passage d'écoulement de fluide (104) au niveau d'un coin (12) où une surface de pression (p), qui configure la surface de pale, vient en contact avec la surface de moyeu (4) dans le voisinage d'une admission (6) du passage d'écoulement de fluide (104),
    caractérisée en ce que le coude (b) est formé dans une région allant d'un bord d'attaque (20) de la pale (3) à une position plus proche du bord d'attaque (20) qu'un bord arrière de la pale (3), et dans une région allant d'une extrémité de moyeu (h) de la pale (3) à une position plus proche de l'extrémité de moyeu (h) qu'une extrémité de pointe (t) de la pale (3).
  2. Roue (1) selon la revendication 1, comprenant en outre
    un second renflement (b') qui est renflé vers l'intérieur du passage d'écoulement de fluide (104) au niveau d'un coin (22) où une surface d'aspiration (n) de la pale (3) vient en contact avec la surface de moyeu (4) dans le voisinage de l'admission (6) du passage d'écoulement de fluide (104).
  3. Machine rotative (100) comprenant la roue (1) selon la revendication 1 ou 2.
EP10799530.0A 2009-07-13 2010-02-18 Roue et machine rotative Not-in-force EP2410186B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2009164782A JP2011021492A (ja) 2009-07-13 2009-07-13 インペラおよび回転機械
PCT/JP2010/001050 WO2011007466A1 (fr) 2009-07-13 2010-02-18 Roue et machine rotative

Publications (3)

Publication Number Publication Date
EP2410186A1 EP2410186A1 (fr) 2012-01-25
EP2410186A4 EP2410186A4 (fr) 2015-05-06
EP2410186B1 true EP2410186B1 (fr) 2017-07-05

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP10799530.0A Not-in-force EP2410186B1 (fr) 2009-07-13 2010-02-18 Roue et machine rotative

Country Status (5)

Country Link
US (1) US9404506B2 (fr)
EP (1) EP2410186B1 (fr)
JP (1) JP2011021492A (fr)
CN (1) CN102365464B (fr)
WO (1) WO2011007466A1 (fr)

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RU2703443C1 (ru) * 2018-02-15 2019-10-16 Эйрбас Хеликоптерс Способ определения первоначальной окружности передней кромки аэродинамических профилей и усовершенствования лопасти с целью увеличения ее отрицательного критического угла атаки

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KR102634097B1 (ko) * 2017-01-06 2024-02-05 한화파워시스템 주식회사 와류 발생 장치를 구비한 임펠러
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Also Published As

Publication number Publication date
JP2011021492A (ja) 2011-02-03
EP2410186A1 (fr) 2012-01-25
WO2011007466A1 (fr) 2011-01-20
CN102365464A (zh) 2012-02-29
EP2410186A4 (fr) 2015-05-06
US9404506B2 (en) 2016-08-02
CN102365464B (zh) 2014-10-29
US20120027599A1 (en) 2012-02-02

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